矩形複合材積層板上に作用する点衝撃の位置および荷重履歴の同定に関する実験的検証 Experimental Verification of Identification of Location and Force History of a Point Impact on Rectangular Composite Laminated Plates

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抄録

Experimental verification of identification of location and force history of a point impact on rectangular composite laminated plates is made in order to establish the identification method proposed previously. In experiments, a point impact on a rectangular composite laminated plate supported at one side was produced by an impulse hammer and the acceleration at points on the surface of the plate was measured by small accelerometers attached on the plate. It is found that by choosing appropriately the number of vibration modes in the identification method, the identification results of the location and force history of the point impact are in good agreement with the exact ones. This may imply that the possibilities of the practical application of the identification method can be expected.

収録刊行物

  • 日本航空宇宙学会論文集 = Journal of the Japan Society for Aeronautical and Space Sciences

    日本航空宇宙学会論文集 = Journal of the Japan Society for Aeronautical and Space Sciences 50(581), 236-241, 2002-06-05

    一般社団法人 日本航空宇宙学会

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被引用文献:  1件中 1-1件 を表示

各種コード

  • NII論文ID(NAID)
    10008840363
  • NII書誌ID(NCID)
    AA11307372
  • 本文言語コード
    JPN
  • 資料種別
    ART
  • ISSN
    13446460
  • NDL 記事登録ID
    6185113
  • NDL 雑誌分類
    ZN25(科学技術--運輸工学--航空機・ロケット)
  • NDL 請求記号
    Z74-B503
  • データ提供元
    CJP書誌  CJP引用  NDL  J-STAGE 
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